DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0872813
Title:
Nonlinear Free Vibrations of Thin, Circular Cylindrical Shells
Descriptive Note:
Final technical rept.
Corporate Author:
STANFORD UNIV CA DEPT OF AERONAUTICS AND ASTRONAUTICS
Report Date:
1970-07-01
Pagination or Media Count:
74.0
Abstract:
The report presents the results of a study of the influence of higher order and nonlinear effects on the free vibration behavior of thin, circular cylindrical shells. A recent solution utilizing strain-displacement relations is examined and criticized. A new solution is carried out which removes the basis for criticism and discloses the existence of a nonperiodic vibration behavior, a phenomenon heretofore unknown. Further, solutions are obtained using strain-displacement relations applied to the shell post-buckling problem. The effect of the improved strain-displacement relations in predicting the vibration behavior attendant to a modal shape possessing a small number of circumferential waves is assessed, and recommendations are made for directing future effort on the problem.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE